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Effect of strain rate on the fracture process in interlaminar shear specimens of carbon fibre-reinforced laminates
Crack detection gauges have been used to determine the start of catastrophic shear failure and to follow its propagation on the interlaminar plane in single-lap shear specimens of unidirectional carbon/epoxy and carbon/PEEK laminates loaded at both quasi-static and impact rates. The interlaminar fai...
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Published in: | Composites. Part A, Applied science and manufacturing Applied science and manufacturing, 1997, Vol.28 (2), p.171-180 |
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Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | Crack detection gauges have been used to determine the start of catastrophic shear failure and to follow its propagation on the interlaminar plane in single-lap shear specimens of unidirectional carbon/epoxy and carbon/PEEK laminates loaded at both quasi-static and impact rates. The interlaminar failure surfaces have been examined using optical and scanning electron microscopy. For carbon/epoxy specimens shear cusps characteristic of mode II shear failure were observed, while for carbon/PEEK specimens a small degree of plastic matrix deformation, typical of fast fracture, was obtained. These results are used to interpret those obtained from the single-lap shear specimen and to discuss the significance of previously published results on the rate dependence of the interlaminar shear strength for carbon/epoxy and carbon/PEEK laminates. |
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ISSN: | 1359-835X 1878-5840 |
DOI: | 10.1016/S1359-835X(96)00112-1 |